EP3524805A1

EP3524805A1 - Engine anomaly detection device

Info

Publication number: EP3524805A1
Application number: EP17909652.4A
Authority: EP
Inventors: Ryo SASE; Shintarou NOGUCHI
Original assignee: Mitsubishi Heavy Industries Engine and Turbocharger Ltd
Current assignee: Mitsubishi Heavy Industries Engine and Turbocharger Ltd
Priority date: 2017-12-27
Filing date: 2017-12-27
Publication date: 2019-08-14
Anticipated expiration: 2037-12-27
Also published as: EP3524805B1; JP6531222B1; EP3524805A4; WO2019130525A1; JPWO2019130525A1; US20200165994A1; CN110199105A

Abstract

An engine abnormality detection device for detecting variation of a combustion state of each of a plurality of cylinders of an engine, the engine abnormality detection device includes: a rotation information acquisition part configured to obtain rotation information related to a rotation state of the engine; a frequency analysis part configured to perform frequency analysis of the rotation information, the frequency analysis part being configured to calculate a component of fand a component fthrough the frequency analysis of the rotation information, where fis a frequency of a single cycle of the engine and fis a frequency of pulsation of the engine; and a detection part configured to detect variation of exhaust energy of each cylinder on the basis of the component of fand the component of f.

Description

TECHNICAL FIELD

The present disclosure relates to an engine abnormality detection device.

BACKGROUND ART

Normally, an automobile engine has a plurality of cylinders. The combustion state of each cylinder may vary due to different causes such as variation of the fuel injection amount or variation of the EGR amount caused by individual difference or aging of injectors, for instance. In particular, in case the combustion state of one of the cylinders deteriorates remarkably, misfire may occur. These abnormalities may lead to malfunction of the engine, and thus it is important to detect these abnormalities in an early stage.
Patent Documents 1 to 6 disclose methods of determining the combustion state of cylinders, such as misfire, from the engine rotation speed or the turbo rotation speed. However, these methods use a rotation speed, which includes noise, and thus cannot always determine the combustion state accurately.
In contrast, Patent Document 7 discloses using a velocity signal that indicates the rotation velocity of the crank shaft and generating an angular acceleration signal that indicates an angular acceleration of the crank shaft to perform frequency analysis of the angular acceleration signal, thereby revealing that the cylinder component of the cylinder frequency of a cylinder with misfire is smaller than the cylinder component of cylinders without misfire. Accordingly, it is possible to determine occurrence of misfire if the cylinder component is smaller than a cylinder threshold, which makes it possible to detect misfire of an engine regardless of noise.

Citation List

Patent Literature

Patent Document 1: JPH3-246353A
Patent Document 2: JP2976684B
Patent Document 3: JP2001-289111A
Patent Document 4: JP2014-234814A
Patent Document 5: JP2016-142181A
Patent Document 6: JP2015-197074A
Patent Document 7: JP2017-106417A

SUMMARY

Problems to be Solved

However, in the method disclosed in Patent Document 7, only misfire is taken into account, and thus it is impossible to effectively detect an abnormality of an injector in which the fuel injection amount to a certain cylinder increases or decreases, and it is also impossible to effectively detect variation of the combustion state of the cylinders caused by a reason other than a change in the fuel injection amount.
In view of the above, an object of at least one embodiment of the present disclosure is to provide an engine abnormality detection device whereby it is possible to detect variation of the combustion state of the cylinders accurately.

Solution to the Problems

(1) According to at least one embodiment of the present invention, an engine abnormality detection device for detecting variation of a combustion state of each of a plurality of cylinders of an engine includes: a rotation information acquisition part configured to obtain rotation information related to a rotation state of the engine; a frequency analysis part configured to perform frequency analysis of the rotation information, the frequency analysis part being configured to calculate a component of f_Ne and a component f_cyl through the frequency analysis of the rotation information, where Ne [rpm] is a rotation speed of the engine, f_Ne [Hz] is a frequency of a single cycle of the engine, satisfying the following expression: $f_{Ne} = \frac{1}{2} \cdot \frac{Ne}{60}$
, n_cyl is the number of the cylinders, and f_cyl [Hz] is a frequency of pulsation of the engine, satisfying the following expression: $f_{cyl} = \frac{1}{2} \cdot \frac{Ne}{60} \cdot n_{cyl}$
; and a detection part configured to detect variation of exhaust energy of each cylinder on the basis of the component of f_Ne and the component of f_cyl.
According to the above configuration (1), by detecting variation of exhaust energy of each of the cylinders on the basis of the component of f_Ne and the component of f_cyl calculated through frequency analysis of the rotation information, it is possible to detect not only a case where the combustion state of a cylinder deteriorates compared to the combustion state of the other cylinders, but also a case where the injection amount of a cylinder is greater than the injection amount of other cylinders or difference in the ignition timing. Thus, it is possible to detect variation of the combustion state of the cylinders accurately.
(2) In some embodiments, in the above configuration (1), for the detection part, a f_Ne threshold being a threshold of the component of f_Ne, and an upper limit threshold f_cyl being an upper limit threshold of the component f_cyl, are set in advance. The detection part is configured to detect that exhaust energy of one of the plurality of cylinders is high, if the component of f_Ne is not smaller than the f_Ne threshold, and the component of f_cyl is not smaller than the f_cyl upper limit threshold.
According to the above configuration (2), through comparison of the component of f_Ne and the f_Ne threshold, and the component of f_cyl and the f_cyl upper limit threshold, it is possible to detect that exhaust energy of one of the plurality of cylinders is high, and thus it is possible to detect variation of the combustion state of the cylinders accurately.
(3) In some embodiments, in the above configuration (1) or (2), for the detection part, a f_Ne threshold being a threshold of the component of f_Ne, and a f_cyl lower limit threshold being a lower limit threshold of the component f_cyl, are set in advance. The detection part is configured to detect that exhaust energy of one of the plurality of cylinder is low, if the component of f_Ne is not smaller than the f_Ne threshold, and the component of f_cyl is not greater than the f_cyl lower limit threshold.
According to the above configuration (3), through comparison of the component of f_Ne and the f_Ne threshold, and the component of f_cyl and the f_cyl lower limit threshold, it is possible to detect that exhaust energy of one of the plurality of cylinders is low, and thus it is possible to detect variation of the combustion state of the cylinders accurately.
(4) In some embodiments, in the above configuration (1), the frequency analysis part is configured to calculate a ratio R of the component of f_Ne to the component of f_cyl (=the component of f_Ne / the component f_cyl) from the calculated component of f_Ne and the calculated component of f_cyl. For the detection part, a threshold of the ratio R is set in advance. The detection part is configured to detect that exhaust energy of one of the plurality of cylinders is low if the ratio R is not smaller than the threshold.
According to the above configuration (4), by utilizing the ratio R of the component of f_Ne and the component of f_cyl, if exhaust energy of one cylinder is low, the component of f_cyl decreases and the component of f_Ne increases. Thus, a change in the ratio R stands out and it is possible to detect a decrease in exhaust energy more accurately.
(5) In some embodiments, in any one of the above configurations (1) to (4), the rotation information is a rotation speed of a turbocharger for supplying compressed intake air to the cylinders.
An engine has a great inertia and thus a change of the rotation speed is less likely to appear, and it is often difficult to detect variation of the combustion state of the cylinders accurately. However, according to the above configuration (5), the rotation speed of the turbocharger is used as the rotation information, and thus a change in the rotation speed of the turbocharger is more likely to appear compared to the engine rotation speed. Thus, it is possible to detect variation of the combustion state of the cylinders accurately.
(6) In some embodiments, in the above configuration (1), the rotation information includes: an engine rotation speed which is a rotation speed of the engine; and a turbo rotation speed which is a rotation speed of a turbocharger for supplying compressed intake air to the cylinders. The frequency analysis part is configured to calculate a component of f_{Ne_Eng} corresponding to the component of f_Ne and a component of f_{cyl_Eng} corresponding to the component of f_cyl through frequency analysis of the engine rotation speed, and calculate a component of f_{Ne_Turbo} corresponding to the component of f_Ne and a component of f_{cyl_Turbo} corresponding to the component of f_cyl through frequency analysis of the turbo rotation speed. The detection part is configured to detect variation of a combustion state of each cylinder on the basis of the component of f_{Ne_Eng}, the component of f_{cyl_Eng}, the component of f_{Ne_Turbo}, and the component of f_{cyl_Turbo}.
According to the above configuration (6), by detecting variation of the combustion state of the cylinders on the basis of the component of f_Ne (the component of f_Ne-Eng and the component of f_Ne-Turbo) and the component of f_cyl (the component of f_cyl-Eng and the component of f_cyl-Turbo) calculated through frequency analysis of the engine rotation speed and the turbo rotation speed, respectively, it is possible to detect variation of the combustion state of the cylinders in more detail compared to a case in which frequency analysis is performed on only one of the engine rotation speed or the turbo rotation speed.
(7) In some embodiments, in the above configuration (6), for the detection part, a f_{Ne_Eng} threshold being a threshold of the component of f_{Ne_Eng}, a f_{cyl_Eng} upper limit threshold being an upper limit threshold of the component of f_{cyl_Eng}, a f_{Ne_Turbo} threshold being a threshold of the component of f_{Ne_Turbo}, and a f_{cyl_Turbo} upper limit threshold being an upper limit threshold of the component of f_{cyl_Turbo}, are set in advance. The detection part is configured to detect that a fuel injection amount to one of the plurality of cylinders is greater than a fuel injection amount to each of the other cylinders, if the component of f_{Ne_Eng} is not smaller than the f_{Ne_Eng} threshold and the component of f_{Ne_Turbo} is not smaller than the f_{Ne_Turbo} threshold, and the component of f_{cyl_Eng} is not smaller than the f_{cyl_Eng} upper limit threshold and the component of f_{cyl_Turbo} is not smaller than the f_{cyl_Turbo} upper limit threshold.
According to the above configuration (7), by comparing the component of f_{Ne_Eng} and the component of f_{Ne_Turbo} to the f_{Ne_Eng} threshold and the f_{Ne_Turbo} threshold respectively, and comparing the component of f_{cyl_Eng} and the component of f_{cyl_Turbo} to the f_{cyl_Eng} upper limit threshold and the f_{cyl_Turbo} upper limit threshold respectively, it is possible to detect that the fuel injection amount to one of the plurality of cylinders is greater than the fuel injection amount to each of the other cylinders. Thus, compared to a case in which frequency analysis is performed on only one of the engine rotation speed or the turbo rotation speed, it is possible to detect the combustion state of the cylinders in more detail.
(8) In some embodiments, in any one of the above configuration (6) or (7), for the detection part, a f_{Ne_Eng} threshold being a threshold of the component of f_{Ne_Eng}, a f_{cyl_Eng} upper limit threshold being an upper limit threshold of the component of f_{cyl_Eng}, a f_{Ne_Turbo} threshold being a threshold of the component of f_{Ne_Turbo}, and a f_{cyl_Turbo} lower limit threshold being a lower limit threshold of the component of f_{cyl_Turbo}, are set in advance. The detection part is configured to detect that a fuel efficiency of one of the cylinders is higher than a fuel efficiency of each of the other cylinders, if the component of f_{Ne_Eng} is not smaller than the f_{Ne_Eng} threshold and the component of f_{Ne_Turbo} is not smaller than the f_{Ne_Turbo} threshold, and the component of f_{cyl_Eng} is not smaller than the f_{cyl_Eng} upper limit threshold and the component of f_{cyl_Turbo} is not greater than the f_{cyl_Turbo} lower limit threshold.
According to the above configuration (8), by comparing the component of f_{Ne_Eng} and the component of f_{Ne_Turbo} to the f_{Ne_Eng} threshold and the f_{Ne_Turbo} threshold respectively, and comparing the component of f_{cyl_Eng} and the component of f_{cyl_Turbo} and the f_{cyl_Eng} upper limit threshold and the f_{cyl_Turbo} lower limit threshold respectively, it is possible to detect that the combustion efficiency of one of the plurality of cylinders is higher than the combustion efficiency of each of the other cylinders. Thus, compared to a case in which frequency analysis is performed on only one of the engine rotation speed or the turbo rotation speed, it is possible to detect the combustion state of the cylinders in more detail.
(9) In some embodiments, in any one of the above configurations (6) to (8), for the detection part, a f_Ne-Eng threshold being a threshold of the component of f_{Ne_Eng}, a f_{cyl_Eng} lower limit threshold being a lower limit threshold of the component of f_{cyl_Eng}, a f_{Ne_Turbo} threshold being a threshold of the component of f_{Ne_Turbo}, and a f_{cyl_Turbo} upper limit threshold being an upper limit threshold of the component of f_{cyl_Turbo}, are set in advance. The detection part is configured to detect that a fuel efficiency of one of the cylinders is lower than a fuel efficiency of each of the other cylinders, if the component of f_{Ne_Eng} is not smaller than the f_{Ne_Eng} threshold and the component of f_{Ne_Turbo} is not smaller than the f_{Ne_Turbo} threshold, and the component of f_{cyl_Eng} is not greater than the f_{cyl_Eng} lower limit threshold and the component of f_{cyl_Turbo} is not smaller than the f_{cyl_Turbo} upper limit threshold.
According to the above configuration (9), by comparing the component of f_{Ne_Eng} and the component of f_{Ne_Turbo} and to f_{Ne_Eng} threshold and the f_{Ne_Turbo} threshold respectively and comparing the component of f_{cyl_Eng} and the component of f_{cyl_Turbo} to the f_{cyl_Eng} lower limit threshold and the f_{cyl_Turbo} upper limit threshold respectively, it is possible to detect that the combustion efficiency of one of the plurality of cylinders is lower than the combustion efficiency of each of the other cylinders. Thus, compared to a case in which frequency analysis is performed on only one of the engine rotation speed or the turbo rotation speed, it is possible to detect the combustion state of the cylinders in more detail.
(10) In some embodiments, in any one of the above configurations (6) to (9), for the detection part, a f_{Ne_Eng} threshold being a threshold of the component of f_{Ne_Eng}, a f_{cyl_Eng} lower limit threshold being a lower limit threshold of the component of f_{cyl_Eng}, a f_{Ne_Turbo} threshold being a threshold of the component of f_{Ne_Turbo}, and a f_{cyl_Turbo} lower limit threshold being a lower limit threshold of the component of f_{cyl_Turbo} are set in advance. The detection part is configured to detect that a fuel injection amount to one of the cylinders is smaller than a fuel injection amount to each of the other cylinders, if the component of f_{Ne_Eng} is not smaller than the f_{Ne_Eng} threshold and the component of f_{Ne_Turbo} is not smaller than the f_{Ne_Turbo} threshold, and the component of f_{cyl_Eng} is not greater than the f_{cyl_Eng} lower limit threshold and the component of f_{cyl_Turbo} is not greater than the f_{cyl_Turbo} lower limit threshold.
According to the above configuration (10), by comparing the component of f_{Ne_Eng} and the component of f_{Ne_Turbo} to the f_{Ne_Eng} threshold and the f_{Ne_Turbo} threshold respectively and comparing the component of f_{cyl_Eng} and the component of f_{cyl_Turbo} to the f_{cyl_Eng} lower limit threshold and the f_{cyl_Turbo} lower limit threshold respectively, it is possible to detect that the fuel injection amount to one of the plurality of cylinders is smaller than the fuel injection amount to each of the other cylinders. Thus, compared to a case in which frequency analysis is performed on only one of the engine rotation speed or the turbo rotation speed, it is possible to detect the combustion state of the cylinders in more detail.
(11) In some embodiments, in any one of the above configurations (2) to (5) and (7) to (10), the engine abnormality detection device further includes: a combustion cylinder identifying part configured to identify a cylinder in which combustion is occurring, of the plurality of cylinders; and an abnormality cylinder identifying part configured to identify the one cylinder on the basis of a result of detection by the detection part and a result of identification by the combustion cylinder identifying part.

According to the above configuration (11), it is possible to identify a cylinder with an abnormal combustion state.

Advantageous Effects

According to at least one embodiment, by detecting variation of exhaust energy of the cylinders on the basis of the component of f_Ne and the component of f_cyl calculated through frequency analysis of the rotation information, it is possible to detect not only a case where the combustion state of a cylinder deteriorates compared to the combustion state of the other cylinders, but also a case where the injection amount of a cylinder is greater than the injection amount of other cylinders or difference in the ignition timing. Thus, it is possible to detect variation of the combustion state of the cylinders accurately.

BRIEF DESCRIPTION OF DRAWINGS

FIG. 1 is a schematic diagram of a configuration of an engine abnormality detection device according to the first embodiment of the present disclosure.
FIG. 2 is a flowchart of an operation of an engine abnormality detection device according to the first embodiment of the present disclosure.
FIG. 3 is a graph showing an example of a relationship between the fuel injection amount to each cylinder, the turbo rotation speed, and the component of f_Ne and the component of f_cyl.
FIG. 4 is a graph showing an example of a relationship between the fuel injection amount to each cylinder, the turbo rotation speed, and the component of f_Ne and the component of f_cyl.
FIG. 5 is a flowchart of an operation of an modified example of an engine abnormality detection device according to the first embodiment of the present disclosure.
FIG. 6 is a flowchart of an operation of another modified example of an engine abnormality detection device according to the first embodiment of the present disclosure.
FIG. 7 is a schematic diagram of a configuration of yet another modified example of an engine abnormality detection device according to the first embodiment of the present disclosure.
FIG. 8 is a flowchart of an operation of an engine abnormality detection device according to the second embodiment of the present disclosure.
FIG. 9 is a schematic diagram of a configuration of an engine abnormality detection device according to the third embodiment of the present disclosure.
FIG. 10 is a matrix for detecting variation of the combustion state for an engine abnormality detection device according to the third embodiment of the present disclosure.

DETAILED DESCRIPTION

Embodiments of the present invention will now be described in detail with reference to the accompanying drawings. However, the scope of the present invention is not limited to the following embodiments. It is intended that dimensions, materials, shapes, relative positions and the like of components described in the embodiments shall be interpreted as illustrative only and not intended to limit the scope of the present invention.

(First embodiment)

FIG. 1 illustrates an in-line four-cylinder engine 1 including four cylinders 2a to 2d arranged in series. An intake pipe 5 is in communication with each of the cylinders 2a to 2d of the engine 1 via an intake manifold 3, and an exhaust pipe 6 is in communication with each of the cylinders 2a to 2d via an exhaust manifold 4. The engine 1 is provided with a turbocharger 9 for supplying compressed intake air to the respective cylinders 2a to 2d. The turbocharger 9 includes a compressor 7 disposed in the intake pipe 5, and a turbine 8 disposed in the exhaust pipe 6.
The engine 1 includes a TDC sensor 11 and a crank angle sensor 12. The turbocharger 9 is provided with a turbo rotation-speed sensor 13 for detecting the turbo rotation speed, which is the rotation speed of the turbocharger 9. The turbo rotation speed is the rotation information related to the rotation state of the engine 1, and thus the turbo rotation-speed sensor 13 constitutes a rotation information acquisition part for obtaining the rotation information related to the rotation state of the engine 1.
An ECU 20, which serves as a control device, includes a frequency analysis part 21 that performs frequency analysis of the turbo rotation speed, which is rotation information related to the rotation state of the engine 1, and a detection part 22 that detects variation of the combustion state of the cylinders 2a to 2d on the basis of the frequency analysis result obtained by the frequency analysis part 21. The turbo rotation-speed sensor 13 is electrically connected to the frequency analysis part 21, and the frequency analysis part 21 and the detection part 22 are connected electrically to each other.
To the detection part 22, a warning part 25 for transmitting a result obtained by the detection part 22 to a driver of a vehicle provided with the engine 1 is connected electrically. The warning part 25 may be a lamp disposed on an instrument panel of the vehicle, a mark or a message that can be shown on the instrument panel, or a speaker that emits a message or a warning sound such as a buzzing sound or music.
Although not an essential configuration in the first embodiment, the ECU 20 may include a combustion cylinder identifying part 23 that identifies a cylinder in which combustion is occurring on the basis of respective detection results of the TDC sensor 11 and the crank angle sensor 12, and an abnormality cylinder identifying part 24 that identifies a cylinder whose combustion state is abnormal on the basis of variation of the combustion state detected by the detection part 22 and the cylinder identified by the combustion cylinder identifying part 23. In a case where the ECU 20 includes the combustion cylinder identifying part 23 and the abnormality cylinder identifying part 24, the TDC sensor 11 and the crank angle sensor 12 are each electrically connected to the combustion cylinder identifying part 23, and the detection part 22 and the combustion cylinder identifying part 23 are each electrically connected to the abnormality cylinder identifying part 24.
Next, the operation of the engine 1 will be described.
When the engine 1 is started, air passes through the intake pipe 5, and is sent to the compressor 7. The air sent to the compressor 7 is compressed by a non-depicted compressor wheel. The compressed air is sent to the intake manifold 3 and is sucked into the four cylinders 2a to 2d periodically. In each of the cylinders 2a to 2d, the compressed air is combusted with fuel and becomes exhaust gas. Exhaust gas discharged from each of the cylinders 2a to 2d is collected in the exhaust manifold 4, and is sent to the turbine 8 through the exhaust pipe 6. The exhaust gas sent to the turbine 8 rotates a non-depicted turbine wheel, and then flows through the exhaust pipe 6 to be discharged into the atmosphere.
Generally, the engine 1 is a four-stroke engine. Thus, two rotations of the engine 1 make up a single cycle. Thus, when Ne [rpm] is the rotation speed of the engine 1, the frequency f_Ne [Hz] of a single cycle of the engine 1 satisfies the following expression: $f_{Ne} = \frac{1}{2} \cdot \frac{Ne}{60}$
Furthermore, when the engine 1 has a plurality of cylinders 2a to 2d, each of the cylinders 2a to 2d combusts once every cycle, and thus, when n_cyl is the number of cylinders (in the engine 1, n_cyl=4), the frequency f_cyl [Hz] of pulsation of the engine 1 satisfies the following expression. $f_{cyl} = \frac{1}{2} \cdot \frac{Ne}{60} \cdot n_{cyl}$
When there is no variation in the combustion state of the cylinders 2a to 2d during operation of the engine 1, pulsation of the engine 1 occurs at the frequency of f_cyl.
In the first embodiment, during operation of the engine 1, presence or absence of variation of the combustion state of the cylinders 2a to 2d is detected. The engine abnormality detection device that detects variation of the combustion state of the cylinders 2a to 2d includes the turbo rotation-speed sensor 13 and the ECU 20.
Next, detection of variation of the combustion state of the cylinders 2a to 2d during operation of the engine 1 will be described on the basis of the flowchart of FIG. 2.
During operation of the engine 1, the turbo rotation-speed sensor 13 detects the turbo rotation speed (step S1), and sends a signal of the turbo rotation speed to the frequency analysis part 21. Next, the frequency analysis part 21 performs the frequency analysis of the signal of the turbo rotation speed, and calculates the component of f_Ne and the component of f_cyl (step S2). Furthermore, as the frequency analysis, a known method may be used, such as fast Fourier transform (FFT).
FIG. 3 is a graph showing an example of a relationship between the fuel injection amount to each of the cylinders 2a to 2d, the turbo rotation speed, and the component of f_Ne and the component of f_cyl. That is, the graph shows a case in which, for two cycles of the engine 1, only the fuel injection amount to the cylinder 2a becomes greater than the fuel injection amount to the other cylinders 2b to 2d, and exhaust energy of the cylinder 2a becomes higher than exhaust energy of the cylinders 2b to 2d. If there is no variation in exhaust energy of the cylinders 2a to 2d, the component of f_cyl, which is the frequency of pulsation of the engine 1, becomes greater than the component of f_Ne. On the other hand, if exhaust energy of the cylinder 2a is higher than exhaust energy of the cylinders 2b to 2d, the amplitude of pulsation of the turbo rotation speed increases, and thus the component of f_cyl increases compared to a case where there is no variation in exhaust energy of the cylinders 2a to 2d. If only exhaust energy of the cylinder 2a becomes high, energy of exhaust gas discharged from the cylinders 2a to 2d loses balance, and thus the component of f_Ne also increases.
FIG. 4 is a graph showing another example of a relationship between the fuel injection amount to each of the cylinders 2a to 2d, the turbo rotation speed, and the component of f_Ne and the component of f_cyl. That is, the graph shows a case where the cylinder 2a misfires in the course of four cycles of the engine 1. If exhaust energy of the cylinder 2a alone decreases due to misfire, the amplitude of pulsation of the turbo rotation speed decreases, and thus the component of f_cyl decreases compared to a case where there is no variation in exhaust energy of the cylinders 2a to 2d. Also, if exhaust energy of the cylinder 2a alone decreases, energy of exhaust gas discharged from the cylinders 2a to 2d loses balance, and thus the component of f_Ne increases. Although an abnormality is occurring in exhaust gas of the cylinder 2a in FIGs. 3 and 4, the result would be the same also in a case where an abnormality occurs in exhaust energy of one of the other cylinders 2b to 2d.
Thus, for the detection part 22 (see FIG. 1), a f_Ne threshold, a f_cyl upper limit threshold and a f_cyl lower limit threshold are set in advance, where a value greater than the component of f_Ne in a case where there is no variation in exhaust energy of the cylinders 2a to 2d is a f_Ne threshold, which is a threshold of the component of f_Ne, and a greater value and a smaller value than the component of f_cyl in a case where there is no variation in exhaust energy of the cylinders 2a to 2d are the f_cyl upper limit threshold, which is the upper limit threshold of the component of f_cyl, and the f_{cyl_}lower limit threshold, which is the lower limit threshold of the component of f_cyl, respectively. Accordingly, if the component of f_Ne is not smaller than the f_Ne threshold and the component of f_cyl is not smaller than the f_cyl upper limit threshold, it can be said that exhaust energy of one of the cylinders 2a to 2d is higher than exhaust energy of the other cylinders. Furthermore, if the component of f_Ne is not smaller than the f_Ne threshold and the component of f_cyl is not greater than the f_cyl lower limit threshold, it can be said that exhaust energy of one of the cylinders 2a to 2d is lower than exhaust energy of the other cylinders.
Furthermore, from such variation of exhaust energy, it is possible to detect variation of the combustion state of the cylinders 2a to 2d (variation of the fuel injection amount, variation of the ignition timing, or deposit adherence or the start of EGR, for instance). The variation of the fuel injection amount or the ignition timing can be corrected on the basis of variation of exhaust energy.
Returning to the flowchart of FIG. 2, in step S3 subsequent to step S2, the detection part 22 determines whether the component of f_Ne is not smaller than the f_Ne threshold. If the component of f_Ne is smaller than the f_Ne threshold, the detection part 22 detects that there is no variation in exhaust energy of the cylinders 2a to 2d, and returns to step S1.
In step S3, if the detection part 22 detects that the component of f_Ne is not smaller than the f_Ne threshold, the detection part 22 determines whether the component of f_cyl is not smaller than the f_cyl upper limit threshold (step S4). If the component of f_cyl is not smaller than the f_cyl upper limit threshold, the detection part 22 detects that exhaust energy of one of the cylinders 2a to 2d is higher than exhaust energy of the other cylinders, and issues a warning of the detection result through the warning part 25 (step S5).
On the other hand, in step S4, if the component of f_cyl is smaller than the f_cyl upper limit threshold, the detection part 22 determines whether the component of f_cyl is not greater than the f_cyl lower limit threshold (step S6). If the component of f_cyl is not greater than the f_cyl lower limit threshold, the detection part 22 detects that exhaust energy of one of the cylinders 2a to 2d is lower than exhaust energy of the other cylinders, and issues a warning of the detection result through the warning part 25 (step S7). In step S6, if the component of f_cyl is not smaller than the f_cyl lower limit threshold, the detection part 22 detects that there is no variation in exhaust energy of the cylinders 2a to 2d, and returns to step S1.
In a case where the ECU 20 includes the combustion cylinder identifying part 23 and the abnormality cylinder identifying part 24, the combustion cylinder identifying part 23 can identify which of the cylinders 2a to 2d combusts at which timing, on the basis of the detection results of the TDC sensor 11 and the crank angle sensor 12. By comparing the timing of combustion of each of the cylinders 2a to 2d and the timing when the component of f_cyl becomes not smaller than the f_cyl upper limit threshold or the timing when the component of f_cyl becomes not greater than the f_cyl lower limit threshold, the abnormality cylinder identifying part 24 can identify in which one of the cylinders 2a to 2d exhaust energy is higher or lower than other cylinders. In this case, by electrically connecting the warning part 25 to the abnormality cylinder identifying part 24, it is possible to issue a warning to inform which of the cylinders has an abnormality of exhaust energy, through the warning part 25.
As described above, by detecting variation of exhaust energy of the cylinders 2a to 2d on the basis of the component of f_Ne and the component of f_cyl calculated through frequency analysis of the turbo rotation speed, it is possible to detect not only a case where the combustion state of a cylinder deteriorates compared to the combustion state of the other cylinders, but also a case where the injection amount of a cylinder is greater than the injection amount of other cylinders or difference in the ignition timing. Thus, it is possible to detect variation of the combustion state of the cylinders 2a to 2d accurately.
In the first embodiment, both of the f_cyl upper limit threshold and the f_cyl lower limit threshold are set in advance for the detection part 22, and the magnitude relationship between the component of f_cyl and both of the f_cyl upper limit threshold and the f_cyl lower limit threshold is determined, to detect both of whether exhaust energy of one of the cylinders 2a to 2d is higher and lower than the other cylinders. Nevertheless, the present invention is not limited to this embodiment. Only the f_cyl upper limit threshold may be set for the detection part 22, and it may be detected only that exhaust energy of one of the cylinders 2a to 2d is higher than exhaust energy of the other cylinders. In this case, as depicted in FIG. 5, if the component of f_cyl is smaller than the f_cyl upper limit threshold in step S4, the procedure returns to step S1. The rest of the operation is the same as that in FIG. 2.
On the other hand, only the f_cyl lower limit threshold may be set for the detection part 22, and it may be detected only that exhaust energy of one of the cylinders 2a to 2d is lower than exhaust energy of the other cylinders. In this case, as depicted in FIG. 6, if the component of f_Ne is not smaller than the f_Ne threshold in step S3, the procedure advances to step S6. The rest of the operation is the same as that in FIG. 2.
In the first embodiment, the turbo rotation speed is used as rotation speed information related to the rotation state of the engine 1. Nevertheless, the rotation speed of the engine 1 (engine rotation speed) may be used as the rotation speed information. The engine rotation speed is detectable with the crank angle sensor 12. Thus, in this case, the crank angle sensor 12 constitutes the rotation information acquisition part. In this modified example, as depicted in FIG. 7, it is not necessary to provide the turbocharger 9 (see FIG. 1) and the turbo rotation-speed sensor 13 (see FIG. 1) and the crank angle sensor 12 is also connected electrically to the frequency analysis part 21. The rest of the configuration is the same as that in FIG. 1. In this case, the engine abnormality detection device includes the crank angle sensor 12 and the ECU 20. The operation in the modified example is the same as that in FIG. 2, except for detecting the engine rotation speed instead of the turbo rotation speed in step S1 of FIG. 2.
However, the engine 1 normally has a great inertia and thus a change of the rotation speed is less likely to appear, and it is often difficult to detect variation of the combustion state of the cylinders 2a to 2d accurately. In contrast, in the first embodiment, the turbo rotation speed is used as the rotation information, and thus a change in the rotation speed of the turbocharger 9 is more likely to appear compared to the engine rotation speed. Thus, compared to a case where the engine rotation speed is used as the rotation information, it is possible to detect variation of the combustion state of the cylinders 2a to 2d accurately.

(Second Embodiment)

Next, the engine abnormality detection device according to the second embodiment will be described. The engine abnormality detection device according to the second embodiment is different from the first embodiment in that the detection operation by the detection part 22 is modified. In the second embodiment, the same constituent elements as those in the first embodiment are associated with the same reference numerals and not described again in detail.
The configuration of the engine abnormality detection device according to the second embodiment is the same as that in FIG.i if the turbo rotation speed is used as the rotational information related to the rotation state of the engine 1, and the same as that in FIG. 7 if the engine rotation speed is used as the rotation information. Hereinafter, in the configuration of FIG. 1, detection of variation of the combustion state of the cylinders 2a to 2d during operation of the engine 1 will be described on the basis of the flow chart of FIG. 8.
The steps S1 and S2 are the same as those in the first embodiment. In step S13 subsequent to step S2, the frequency analysis part 21 calculates a ratio R (= the component of f_Ne / the component of f_cyl) of the component of f_Ne to the component of f_cyl from the calculated components. The detection part 22 has a threshold of the ratio R set in advance. In step 14 subsequent to step S13, the detection part 22 determines whether the ratio R is not smaller than the threshold. If the ratio R is smaller than the threshold, the detection part 22 detects that there is no variation in exhaust energy of the cylinders 2a to 2d, and returns to step S1. If the ratio R is not smaller than the threshold in step S14, the detection part 22 detects that exhaust energy of one of the cylinders 2a to 2d is low, and issues a warning of the detection result through the warning part 25 (step S15).
In the second embodiment, by utilizing the ratio R of the component of f_Ne to the component of f_cyl, if exhaust energy of one cylinder is low, the component of f_cyl decreases and the component of f_Ne increases. Thus, a change in the ratio R stands out and it is possible to detect a change in exhaust energy accurately.

(Third Embodiment)

Next, the engine abnormality detection device according to the third embodiment will be described. The engine abnormality detection device according to the third embodiment is different from the first embodiment in that the detection operation by the detection part 22 is modified. In the third embodiment, the same constituent elements as those in the first embodiment are associated with the same reference numerals and not described again in detail.
As depicted in FIG. 9, the configuration of the engine abnormality detection device according to the third embodiment is the same as that of the first embodiment, except that the crank angle sensor 12 is also electrically connected to the frequency analysis part 21.
Next, detection of variation of the combustion state of each of the cylinders 2a to 2d during operation of the engine 1 will be described.
In the third embodiment, both of the turbo rotation speed and the engine rotation speed are used as rotation speed information related to the rotation state of the engine 1. The frequency analysis part 21 performs frequency analysis of each of the turbo rotation speed and the engine rotation speed, to calculate the component of f_Ne-Turbo and the component of f_cyl-Turbo corresponding to the component of f_Ne and the component of f_cyl in the first embodiment from the turbo rotation speed, and calculate the component of f_Ne-Eng and the component of f_cyl-Eng corresponding to the component of f_Ne and the component of f_cyl in the first embodiment from the engine rotation speed.
Then, the operation from step S3 to step S7 of the first embodiment is performed on each of the component of f_Ne-Turbo and the component of f_cyl-Turbo, and the component of f_Ne-Eng and the component of f_cyl-Eng (see FIG. 2). For determination in step S3, step S4, and step S6, the detection part 22 includes the following thresholds that are set in advance: the f_Ne-Turbo threshold and the f_Ne-Eng threshold which are thresholds of the component of f_Ne-Turbo and the component of f_{Ne_Eng}, respectively; the f_cyl-Turbo upper limit threshold and the f_cyl-Turbo lower limit threshold, which are an upper limit threshold and a lower limit threshold of the component of f_cyl-Turbo; and the f_cyl-Eng upper limit threshold and the f_cyl-Eng lower limit threshold which are an upper limit threshold and a lower limit threshold of the component of f_cyl-Eng.
If there is variation in the combustion state of the cylinders 2a to 2d, it is determined, through the above operation, that the component of f_Ne-Turbo and the component of f_cyl-Turbo are not smaller than the threshold of f_Ne-Turbo and the threshold of f_{Ne_Eng}, and satisfy one of the following determination result.

(1) The component of f_cyl-Turbo is not smaller than the f_cyl-Turbo upper limit threshold, and the component of f_cyl-Eng is not smaller than the f_cyl-Eng upper limit threshold.
(2) The component of f_cyl-Turbo is not greater than the f_cyl-Turbo lower limit threshold, and the component of f_cyl-Eng is not smaller than the f_cyl-Eng upper limit threshold.
(3) The component of f_cyl-Turbo is not smaller than the f_cyl-Turbo upper limit threshold, and the component of f_cyl-Eng is not greater than the f_cyl-Eng lower limit threshold.
(4) The component of f_cyl-Turbo is not greater than the f_cyl-Turbo lower limit threshold, and the component of f_cyl-Eng is not greater than the f_cyl-Eng lower limit threshold.

If the above determination result (1) is satisfied, it is detected that the fuel injection amount to one cylinder is greater than the fuel injection amount to each of the other cylinders. If the above determination result (2) is satisfied, it is detected that the combustion efficiency of one cylinder is greater than the combustion efficiency of each of the other cylinders. If the above determination result (3) is satisfied, it is detected that the combustion efficiency of one cylinder is smaller than the combustion efficiency of each of the other cylinders. If the above determination result (4) is satisfied, it is detected that the fuel injection amount to one cylinder is smaller than the fuel injection amount to each of the other cylinders.
FIG. 10 is a matrix indicating a relationship between the determination results (1) to (4) and the aspects of variation of the combustion state corresponding thereto. With the matrix being incorporated into the detection part 22 (FIG. 9) in advance, it is possible to detect the aspects of variation of the combustion state on the basis of the determination results (1) to (4), and issue a warning of the detection result through the warning part 25.
As described above, by detecting variation of the combustion state of the cylinders on the basis of the component of f_Ne-Eng and the component of f_Ne-Turbo and the component of f_cyl-Eng and the component of f_cyl-Turbo calculated through frequency analysis of each of the engine rotation speed and the turbo rotation speed, it is possible to detect variation of the combustion state of the cylinders 2a to 2d in more detail compared to a case in which frequency analysis is performed on only one of the engine rotation speed or the turbo rotation speed.
In the third embodiment, similarly to the first embodiment, with the ECU 20 including the combustion cylinder identifying part 23 and the abnormality cylinder identifying part 24, it is possible to determine in which of the cylinders 2a to 2d the detected variation of the combustion state is occurring.
In the third embodiment, for the detection part 22, the f_Ne-Turbo threshold and the f_Ne-Eng threshold, the f_cyl-Turbo upper limit threshold and the f_cyl-Turbo lower limit threshold, the f_cyl-Eng upper limit threshold and the f_cyl-Eng lower limit threshold are set in advance, and it is determined which one of the determination results (1) to (4) is satisfied. Nevertheless, the present invention is not limited to this embodiment. For instance, only necessary thresholds may be set for the detection part 22, and only one, two, or three of the determination results (1) to (3) may be determined. For instance, the f_Ne-Turbo threshold and the f_Ne-Eng threshold, and the f_cyl-Turbo upper limit threshold and the f_cyl-Eng upper limit threshold may be set for the detection part 22 to determine only whether the determination result (1) is satisfied.
While the engine 1 is an in-line four-cylinder engine in the first to third embodiments, the present invention is not limited to these embodiments. The engine 1 may be a V-type engine, or a horizontally-opposed cylinder engine. Further, the engine is not limited to the configuration including four cylinders, and may be of any type as long as the engine includes two or more cylinders.

Description of Reference Numerals

1: Engine
2a: Cylinder
2b: Cylinder
2c: Cylinder
2d: Cylinder
3: Intake manifold
4: Exhaust manifold
5: Intake pipe
6: Exhaust pipe
7: Compressor
8: Turbine
9: Turbocharger
11: TDC sensor
12: Crank angle sensor (rotation information acquisition part)
13: Turbo rotation-speed sensor (rotation information acquisition part)
20: ECU
21: Frequency analysis part
22: Detection part
23: Combustion cylinder identifying part
24: Abnormality cylinder identifying part
25: Warning part

Claims

An engine abnormality detection device for detecting variation of a combustion state of each of a plurality of cylinders of an engine, the engine abnormality detection device comprising:
a rotation information acquisition part configured to obtain rotation information related to a rotation state of the engine;

a frequency analysis part configured to perform frequency analysis of the rotation information, the frequency analysis part being configured to calculate a component of f_Ne and a component f_cyl through the frequency analysis of the rotation information, where Ne [rpm] is a rotation speed of the engine, f_Ne [Hz] is a frequency of a single cycle of the engine, satisfying the following expression: $f_{Ne} = \frac{1}{2} \cdot \frac{Ne}{60}$
, n_cyl is the number of the cylinders, and f_cyl[Hz] is a frequency of pulsation of the engine, satisfying the following expression: $f_{cyl} = \frac{1}{2} \cdot \frac{Ne}{60} \cdot n_{cyl}$
; and

a detection part configured to detect variation of exhaust energy of each cylinder on the basis of the component of f_Ne and the component of f_cyl.
The engine abnormality detection device according to claim 1,
wherein, for the detection part,
a f_Ne threshold being a threshold of the component of f_Ne, and
an upper limit threshold f_cyl being an upper limit threshold of the component f_cyl,
are set in advance, and
wherein the detection part is configured to detect that exhaust energy of one of the plurality of cylinders is high, if the component of f_Ne is not smaller than the f_Ne threshold, and the component of f_cyl is not smaller than the f_cyl upper limit threshold.
The engine abnormality detection device according to claim 1 or 2,
wherein, for the detection part,
a f_Ne threshold being a threshold of the component of f_Ne, and
a f_cyl lower limit threshold being a lower limit threshold of the component f_cyl,
are set in advance, and
wherein the detection part is configured to detect that exhaust energy of one of the plurality of cylinder is low, if the component of f_Ne is not smaller than the f_Ne threshold, and the component of f_cyl is not greater than the f_cyl lower limit threshold.
The engine abnormality detection device according to claim 1,
wherein the frequency analysis part is configured to calculate a ratio R of the component of f_Ne to the component of f_cyl (=the component of f_Ne / the component f_cyl) from the calculated component of f_Ne and the calculated component of f_cyl,
wherein, for the detection part, a threshold of the ratio R is set in advance, and
wherein the detection part is configured to detect that exhaust energy of one of the plurality of cylinders is low if the ratio R is not smaller than the threshold.
The engine abnormality detection device according to any one of claims 1 to 4,
wherein the rotation information is a rotation speed of a turbocharger for supplying compressed intake air to the cylinders.
The engine abnormality detection device according to claim 1,
wherein the rotation information includes:
an engine rotation speed which is a rotation speed of the engine; and

a turbo rotation speed which is a rotation speed of a turbocharger for supplying compressed intake air to the cylinders,

wherein the frequency analysis part is configured to calculate a component of f_{Ne_Eng} corresponding to the component of f_Ne and a component of f_{cyl_Eng} corresponding to the component of f_cyl through frequency analysis of the engine rotation speed, and calculate a component of f_{Ne_Turbo} corresponding to the component of f_Ne and a component of f_{cyl_Turbo} corresponding to the component of f_cyl through frequency analysis of the turbo rotation speed, and

wherein the detection part is configured to detect variation of a combustion state of each cylinder on the basis of the component of f_{Ne_Eng}, the component of f_{cyl_Eng}, the component of f_{Ne_Turbo}, and the component of f_{cyl_Turbo}.
The engine abnormality detection apparatus according to claim 6,
wherein, for the detection part,
a f_{Ne_Eng} threshold being a threshold of the component of f_{Ne_Eng},
a f_{cyl_Eng} upper limit threshold being an upper limit threshold of the component of f_{cyl_Eng},
a f_{Ne_Turbo} threshold being a threshold of the component of f_{Ne_Turbo}, and
a f_{cyl_Turbo} upper limit threshold being an upper limit threshold of the component of f_{cyl_Turbo},
are set in advance, and
wherein the detection part is configured to detect that a fuel injection amount to one of the plurality of cylinders is greater than a fuel injection amount to each of the other cylinders, if the component of f_{Ne_Eng} is not smaller than the f_{Ne_Eng} threshold and the component of f_{Ne_Turbo} is not smaller than the f_{Ne_Turbo} threshold, and the component of f_{cyl_Eng} is not smaller than the f_{cyl_Eng} upper limit threshold and the component of f_{cyl_Turbo} is not smaller than the f_{cyl_Turbo} upper limit threshold.
The engine abnormality detection apparatus according to claim 6 or 7,
wherein, for the detection part,
a f_{Ne_Eng} threshold being a threshold of the component of f_{Ne_Eng},
a f_{cyl_Eng} upper limit threshold being an upper limit threshold of the component of f_{cyl_Eng},
a f_{Ne_Turbo} threshold being a threshold of the component of f_{Ne_Turbo}, and
a f_{cyl_Turbo} lower limit threshold being a lower limit threshold of the component of f_{cyl_Turbo},
are set in advance, and
wherein the detection part is configured to detect that a fuel efficiency of one of the cylinders is higher than a fuel efficiency of each of the other cylinders, if the component of f_Ne-Eng is not smaller than the f_Ne-Eng threshold and the component of f_{Ne_Turbo} is not smaller than the f_{Ne_Turbo} threshold, and the component of f_{cyl_Eng} is not smaller than the f_{cyl_Eng} upper limit threshold and the component of f_{cyl_Turbo} is not greater than the f_{cyl_Turbo} lower limit threshold.
The engine abnormality detection apparatus according to any one of claims 6 to 8,
wherein, for the detection part,
a f_{Ne_Eng} threshold being a threshold of the component of f_{Ne_Eng},
a f_{cyl_Eng} lower limit threshold being a lower limit threshold of the component of f_{cyl_Eng},
a f_{Ne_Turbo} threshold being a threshold of the component of f_{Ne_Turbo}, and
a f_{cyl_Turbo} upper limit threshold being an upper limit threshold of the component of f_{cyl_Turbo},
are set in advance, and
wherein the detection part is configured to detect that a fuel efficiency of one of the cylinders is lower than a fuel efficiency of each of the other cylinders, if the component of f_{Ne_Eng} is not smaller than the f_{Ne_Eng} threshold and the component of f_{Ne_Turbo} is not smaller than the f_{Ne_Turbo} threshold, and the component of f_{cyl_Eng} is not greater than the f_{cyl_Eng} lower limit threshold and the component of f_{cyl_Turbo} is not smaller than the f_{cyl_Turbo} upper limit threshold.
The engine abnormality detection apparatus according to any one of claims 6 to 9,
wherein, for the detection part,
a f_{Ne_Eng} threshold being a threshold of the component of f_{Ne_Eng},
a f_{cyl_Eng} lower limit threshold being a lower limit threshold of the component of f_{cyl_Eng},
a f_{Ne_Turbo} threshold being a threshold of the component of f_{Ne_Turbo}, and
a f_{cyl_Turbo} lower limit threshold being a lower limit threshold of the component of f_{cyl_Turbo},
are set in advance, and
wherein the detection part is configured to detect that a fuel injection amount to one of the cylinders is smaller than a fuel injection amount to each of the other cylinders, if the component of f_{Ne_Eng} is not smaller than the f_{Ne_Eng} threshold and the component of f_{Ne_Turbo} is not smaller than the f_{Ne_Turbo} threshold, and the component of f_{cyl_Eng} is not greater than the f_{cyl_Eng} lower limit threshold and the component of f_{cyl_Turbo} is not greater than the f_{cyl_Turbo} lower limit threshold.
The engine abnormality detection device according to any one of claims 2 to 5 and 7 to 10, further comprising:
a combustion cylinder identifying part configured to identify a cylinder in which combustion is occurring, of the plurality of cylinders; and

an abnormality cylinder identifying part configured to identify the one cylinder on the basis of a result of detection by the detection part and a result of identification by the combustion cylinder identifying part.